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CrN/AlN superlattice coatings synthesized by pulsed closed field unbalanced magnetron sputtering with different CrN layer thicknesses
Authors:Jianliang Lin  John J Moore  Malki Pinkas  William D Sproul
Affiliation:a Advanced Coatings and Surface Engineering Laboratory (ACSEL), Colorado School of Mines, Golden, Colorado, 80401, USA
b Nuclear Research Center, Negev, Israel
c Reactive Sputtering, INC, 2152 Goya Place, San Marcos, California, USA
Abstract:CrN/AlN superlattice coatings with different CrN layer thicknesses were prepared using a pulsed closed field unbalanced magnetron sputtering system. A decrease in the bilayer period from 12.4 to 3.0 nm and simultaneously an increase in the Al/(Cr + Al) ratio from 19.1 to 68.7 at.% were obtained in the CrN/AlN coatings when the Cr target power was decreased from 1200 to 200 W. The bilayer period and the structure of the coatings were characterized by means of low angle and high angle X-ray diffraction and transmission electron microscopy. The mechanical and tribological properties of the coatings were studied using the nanoindentation and ball-on-disc wear tests. It was found that CrN/AlN superlattice coatings synthesized in the current study exhibited a single phase face-centered cubic structure with well defined interfaces between CrN and AlN nanolayers. Decreases in the residual stress and the lattice parameter were identified with a decrease in the CrN layer thickness. The hardness of the coatings increased with a decrease in the bilayer period and the CrN layer thickness, and reached the highest value of 42 GPa at a bilayer period of 4.1 nm (CrN layer thickness of 1.5 nm, AlN layer thickness of 2.5 nm) and an Al/(Cr + Al) ratio of 59.3 at.% in the coatings. A low coefficient of friction of 0.35 and correspondingly low wear rate of 7 × 10− 7 mm3N− 1m− 1 were also identified in this optimized CrN/AlN coating when sliding against a WC-6%Co ball.
Keywords:Superlattice coatings  CrN/AlN  Pulsed magnetron sputtering  CrAlN  Wear
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